Unsteady separation in flare-induced hypersonic shock-wave boundary-layer interaction flowfield

Journal of Spacecraft and Rockets

Volumn 39, Issue 3, 2002, Pages 467-470

  Verma, Shashi B ^a,b   Koppenwallner, G ^a,c  

^a HTG Hyperschall Technologie Gottingen   (Germany)

^b Langer Grund   (Germany)

^c Aerodynamics Division   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIR; BOUNDARY LAYER FLOW; CALIBRATION; DATA ACQUISITION; ELECTRIC POTENTIAL; FLOW VISUALIZATION; HIGH PRESSURE EFFECTS; HYPERSONIC FLOW; IMAGING TECHNIQUES; LASER THEORY; OSCILLATIONS; PHOTODIODES; SCHLIEREN SYSTEMS; SPACE SHUTTLES; TRANSDUCERS;

MACH NUMBERS; SHOCK-WAVE BOUNDARY LAYER INTERACTIONS (SWBLI);

SHOCK WAVES;

EID: 0036576934     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3831     Document Type: Article

References (10)

1. Fluctuating wall pressure under a separated supersonic flow
2. Unsteadiness of the separation shock wave structure in a supersonic compression ramp field
3. Hypersonic flow over axially symmetric spiked bodies
4. An experimental investigation of the unsteady behaviour of blunt fin-induced shock wave turbulent boundary layer interaction
5. New diagnostic technique for the study of turbulent boundary layer separation
6. Experimental study of shock unsteadiness on an hyperboloid model using laser schlieren
7. Calibration and first results of redesigned ludwieg expansion tube
8. Laser schlieren cross-beam measurements in a supersonic jet shear layer
9. Unsteady pressure loads generated by swept-shock-wave/boundary-layer interactions
10. Stagnation point fluctuations on a body of revolution